{"created":"2023-06-20T15:10:44.326223+00:00","id":40312,"links":{},"metadata":{"_buckets":{"deposit":"0a52e6bd-45f4-488a-86a1-afe860713ed4"},"_deposit":{"created_by":1,"id":"40312","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"40312"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00040312","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["447281","447276","447277","447278","447280","447279"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Conceptional study for improving the efficiency of the return flight path design of the space shuttle"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-10","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"28","bibliographicPageStart":"1","bibliographicVolumeNumber":"1365","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"宇宙往還機の再突入以降の帰還経路は、帰還飛行経路を再突入・エネルギー調整・進入着陸の3つのフェーズに分割し、各フェーズ間のインタフェース条件を仮定した上で、設計された誘導則をもとに各フェーズの飛行経路を個別に計算し、インタフェース点における各パラメータ値の差を最小とするよう繰り返し計算して求めるのが一般的である。本研究では、帰還飛行経路を飛行フェーズに分割し繰り返し計算により求めるのでなく、再突入から着陸点近傍までの飛行経路を機体の揚抗比で定まる帰還飛行時の滑空性能から、包括的に把握する手法を検討し、帰還飛行経路の存在域を回廊として求めるアルゴリズムの開発を行うものである。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The return flight path of the space shuttle used to be designed through parametric iteration to reduce the gaps at the interface points of the two adjacent flight paths, of different flight phases of reentry, TAEM (Terminal Area Energy Management) and AL (Approach Landing), which are maneuvered by the guidance program. This research shows that the return flight path can be deduced from the gliding performance, which is determined by the Lift/Drag ratio (L/D), where L/D is controlled by the angle of attack, the speed brake angle and the bank angle, and that an algorithm to determine the return flight path corridor depending on the gliding capability of the vehicle can be derived.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001672000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TR-1365","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 新型航空機研究グループ"},{"subitem_text_value":"航空宇宙技術研究所 新型航空機研究グループ"},{"subitem_text_value":"航空宇宙技術研究所 宇宙研究グループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Aircraft Research Group"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Aircraft Research Group"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Space Technology Research Group"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"原, 裕二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"伊藤, 婦美子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"末松, 俊二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hara, Yasuji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ito, Fumiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suematsu, Shunji","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-27"}],"displaytype":"detail","filename":"naltr0001365.pdf","filesize":[{"value":"1.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001365.pdf","url":"https://jaxa.repo.nii.ac.jp/record/40312/files/naltr0001365.pdf"},"version_id":"435ffc62-3ac1-40bd-afe6-dde3b332fa26"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"帰還飛行","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙往還機","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行経路","subitem_subject_scheme":"Other"},{"subitem_subject":"大気圏再突入","subitem_subject_scheme":"Other"},{"subitem_subject":"揚抗比","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行経路角","subitem_subject_scheme":"Other"},{"subitem_subject":"ダイナミックパス","subitem_subject_scheme":"Other"},{"subitem_subject":"進入着陸経路","subitem_subject_scheme":"Other"},{"subitem_subject":"回廊","subitem_subject_scheme":"Other"},{"subitem_subject":"return flight","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space shuttle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight path","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"atmosphere reentry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lift to drag ratio","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight path angle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic path","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"approach landing path","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"corridor","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"宇宙往還機帰還経路設計開発の効率化概念検討","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"宇宙往還機帰還経路設計開発の効率化概念検討"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"40312","relation_version_is_last":true,"title":["宇宙往還機帰還経路設計開発の効率化概念検討"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:15:36.158942+00:00"}